| 100 - Two 1490kW (2000shp) Pratt & Whitney Canada PW120A turboprops driving four blade constant speed Hamilton Standard propellers. 100B - Two 1605kW (2150shp) PW121As. 200 - Two 1605kW (2150shp) PW123Cs in 200A, or two PW123Ds in 200B. |
| Performance |
|---|
|
100A - Max cruising speed 490km/h (265kt), long range cruising speed 440km/h (237kt). Initial rate of climb 1560ft/min. Range with full passenger load, fuel and reserves 1520km (820nm), range with a 2720kg (6000lb) payload 2040km (1100nm). 100B - Same except max cruising speed of 500km/h (270kt). 200A & 200B - Same except max cruising speed 546km/h (295kt). Initial rate of climb 1475ft/min. Range with 37 passengers 1795km (970nm).
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| Weights |
|---|
| 100A - Operating empty 10,250kg (22,600lb), max takeoff 15,650kg (34,500lb). 100B - Operating empty 10,273kg (22,648lb), max takeoff 16,465kg (36,300lb). 200A & 200B - Operating empty 10,434kg (23,004lb), max takeoff 16,465kg (36,300lb).
|
| Dimensions |
|---|
| Wing span 25.91m (85ft 0in), length 22.25m (73ft 0in), height 7.49m (24ft 7in). Wing area 54.4m2 (585.0sq ft).
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| Capacity |
|---|
| Flightcrew of two. Typical passenger seating for 37 at four abreast and 79cm (31in) pitch, max seating for 40.
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